CN206700758U - A kind of wing of model aircraft - Google Patents
A kind of wing of model aircraft Download PDFInfo
- Publication number
- CN206700758U CN206700758U CN201720351774.8U CN201720351774U CN206700758U CN 206700758 U CN206700758 U CN 206700758U CN 201720351774 U CN201720351774 U CN 201720351774U CN 206700758 U CN206700758 U CN 206700758U
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- China
- Prior art keywords
- wing
- rod
- narrow
- wide
- longitudinal
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Abstract
It the utility model is related to a kind of wing of model aircraft, including wing, longitudinally longitudinally the wide body of rod, the wing transverse direction body of rod, wing connect the narrow body of rod, wing connects the wide body of rod for the narrow body of rod, wing, wing connects the terminal position that the narrow body of rod is connected to the longitudinal longitudinal wide body of rod of the narrow body of rod and wing of wing, the wing transverse direction body of rod is connected to the front position of the longitudinal longitudinal wide body of rod of the narrow body of rod and wing of wing, and wing connects the centre position that the wide body of rod is connected to the longitudinal longitudinal wide body of rod of the narrow body of rod and wing of wing；Two huge linkage holes are machined with the end face of the wing transverse direction body of rod, three small connecting holes are machined with the end face of the wing transverse direction body of rod, fastener is installed in two huge linkage holes and three small connecting holes so as to which wing is arranged on fuselage.The utility model is by being provided with three hollow out connecting rod A and two hollow out connecting rod B, it is possible to increase its structural strength, by being provided with two huge linkage holes and three small connecting holes, is easy to install whole wing.
Description
Technical field
It the utility model is related to model aircraft technical field, more particularly to a kind of wing of model aircraft.
Background technology
Model aircraft is different from the model of an airplane, and model aircraft is normally only used for decorating, shown, it is not possible to fly, be with
The model that aircraft reduces by a certain percentage for image.And the model of an airplane refers to fly and can be realized by modes such as remote controls
A kind of toy of control to aircraft.
Static model aircraft material has a variety of, has metal, plastics, resin, fiberglass etc., is proportionally also classified into more than 10 lis
Rice, more than 20 centimetres, more than 30 centimetres, more than 40 centimetres, until the model more than one meter.Prominent domestic has, destroy -10 model aircrafts, destroy -
15 carrier-borne aircraft models, -20 model aircrafts are destroyed, -11/ is destroyed and destroys -11B model aircrafts etc..
Dynamic airplane model also has a variety of, and main making material is：EPP foam, EPO foams, KT sheet material matter etc..Dynamic flies
Machine model can fly, predominantly telecontrolled aircraft model, by artificially passing through remote control control heading and speed.Flying power
Typically realized by battery or gasoline.
Model aircraft is applied to popularization exhibitions at present, the main element such as wing, vertical fin and horizontal tail on model aircraft with
Model aircraft is overall in one, not easy to remove, in transport, easily damages, while the wing on model aircraft is in use
It is easily damaged.
Utility model content
The purpose of this utility model is for overcome the deficiencies in the prior art, there is provided a kind of wing of model aircraft.
The utility model is to be achieved through the following technical solutions：
A kind of wing of model aircraft, including the longitudinal narrow body of rod, the wing longitudinally wide body of rod, the wing transverse direction body of rod, the machine of wing
The wing connects the narrow body of rod, wing connects the wide body of rod, and the narrow body of rod of described wing connection is connected to wing, and longitudinally narrow the body of rod and wing are indulged
To the terminal position of the wide body of rod, the described wing transverse direction body of rod is connected to the wing longitudinally narrow body of rod and wing longitudinally before the wide body of rod
End position, described wing connect the centre position that the wide body of rod is connected to the longitudinal longitudinal wide body of rod of the narrow body of rod and wing of wing；
Two huge linkage holes are machined with the end face of the wing transverse direction body of rod, three are machined with the end face of the wing transverse direction body of rod
Individual small connecting hole, fastener is installed in two huge linkage holes and three small connecting holes so as to which wing is arranged on fuselage.
Further, in described wing, longitudinally narrow the body of rod and wing are longitudinally provided with three hollow outs connections between the wide body of rod
Bar A.
Further, in described wing, longitudinally narrow the body of rod and wing are longitudinally provided with two hollow outs connections between the wide body of rod
Bar B.
Further, longitudinally longitudinally the wide body of rod, the wing transverse direction body of rod, wing connection are narrow for the narrow body of rod, wing for described wing
The body of rod and wing connect the wide body of rod and are integrally formed setting, and the longitudinal narrow body of rod, the wing longitudinally wide body of rod, the wing of described wing
The horizontal body of rod, wing connect the narrow body of rod, wing connects the wide body of rod, three hollow out connecting rod A and two hollow out connecting rod B and adopted
It is made of otherwise identical plastic material.
Compared with prior art, the beneficial effects of the utility model are：The utility model is streamlined knot when in use
Structure, higher fidelity is realized on aerodynamic configuration, by being provided with three hollow out connecting rod A and two hollow out connecting rod B, energy
Its structural strength is enough improved, by being provided with two huge linkage holes and three small connecting holes, is easy to that whole wing is installed.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Embodiment
In order that the purpose of this utility model, technical scheme and advantage are more clearly understood, below in conjunction with accompanying drawing and implementation
Example, the utility model is further elaborated.It should be appreciated that specific embodiment described herein is only explaining
The utility model, it is not used to limit the utility model.
Referring to Fig. 1, Fig. 1 is structural representation of the present utility model.
A kind of wing of described model aircraft, including longitudinally longitudinally the wide body of rod 2, wing are horizontal for the narrow body of rod 1, wing for wing
The body of rod 3, wing connect the narrow body of rod 4, wing connects the wide body of rod 5, and described wing connects the narrow body of rod 4 and is connected to wing longitudinally narrow bar
The terminal position of the longitudinal wide body of rod 2 of body 1 and wing, the described wing transverse direction body of rod 3 are connected to the wing longitudinally narrow body of rod 1 and wing
The front position of the wide body of rod 2 in longitudinal direction, described wing connect the wide body of rod 5 and are connected to the wing longitudinally narrow body of rod 1 and wing longitudinal direction width
The centre position of the body of rod 2；Two huge linkage holes 6 are machined with the end face of the wing transverse direction body of rod 3, it is horizontal in the wing
Three small connecting hole 7 is machined with the end face of the body of rod 3, fastener is installed in two huge linkage holes 6 and three small connecting hole 7
So as to which wing is arranged on fuselage.
In described wing, longitudinally narrow the body of rod 1 and wing are longitudinally provided with three hollow out connecting rod A8 between the wide body of rod 2,
Longitudinally the narrow body of rod 1 and wing are longitudinally provided with two hollow out connecting rod B9 between the wide body of rod 2 to described wing.Described wing is indulged
To the narrow body of rod 1, wing, longitudinally the wide body of rod 2, the wing transverse direction body of rod 3, wing connect the wide body of rod 5 one of the narrow body of rod 4 and wing connection
Body formed setting, and longitudinally longitudinally the wide body of rod 2, the wing transverse direction body of rod 3, wing connect narrow bar to described wing for the narrow body of rod 1, wing
Body 4, wing connect wide 5, three hollow out connecting rod A8 of the body of rod and two hollow out connecting rod B9 and use otherwise identical plastic material system
Into.
The utility model when in use, is streamlined structure, higher fidelity is realized on aerodynamic configuration, by being provided with
Three hollow out connecting rod A8 and two hollow out connecting rod B9, it is possible to increase its structural strength, by being provided with two big connection
Hole 6 and three small connecting hole 7, are easy to install whole wing.
In description of the present utility model, unless otherwise clearly defined and limited, term " installation ", " connected ", " company
Connect " it should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integrally；It can be direct phase
Even, it can also be indirectly connected by intermediary, can be that the connection of two element internals or the interaction of two elements are closed
System.For the ordinary skill in the art, it can understand that above-mentioned term is specific in the utility model with concrete condition
Implication.
Preferred embodiment of the present utility model is the foregoing is only, it is all at this not to limit the utility model
All any modification, equivalent and improvement made within the spirit and principle of utility model etc., should be included in the utility model
Protection domain within.
Claims (4)
- A kind of 1. wing of model aircraft, it is characterised in that：Including wing longitudinally the narrow body of rod (1), wing longitudinally the wide body of rod (2), The wing transverse direction body of rod (3), wing connect the narrow body of rod (4), wing connects the wide body of rod (5), and described wing connects the narrow body of rod (4) even It is connected on the terminal position of the longitudinal longitudinal wide body of rod (2) of the narrow body of rod (1) and wing of wing, the connection of the described wing transverse direction body of rod (3) In the front position of the longitudinal longitudinal wide body of rod (2) of the narrow body of rod (1) and wing of wing, described wing connects the wide body of rod (5) connection In the centre position of the longitudinal longitudinal wide body of rod (2) of the narrow body of rod (1) and wing of wing；In the end face of the wing transverse direction body of rod (3) On be machined with two huge linkage holes (6), three small connecting hole (7) is machined with the end face of the wing transverse direction body of rod (3), Fastener is installed so as to which wing is arranged on fuselage in two huge linkage holes (6) and three small connecting hole (7).
- A kind of 2. wing of model aircraft according to claim 1, it is characterised in that：In the longitudinal narrow body of rod of described wing (1) and wing is longitudinally provided with three hollow out connecting rod A (8) between the wide body of rod (2).
- A kind of 3. wing of model aircraft according to claim 2, it is characterised in that：In the longitudinal narrow body of rod of described wing (1) and wing is longitudinally provided with two hollow out connecting rod B (9) between the wide body of rod (2).
- A kind of 4. wing of model aircraft according to claim 3, it is characterised in that：The longitudinal narrow body of rod of described wing (1), longitudinally the wide body of rod (2), the wing transverse direction body of rod (3), wing connect the narrow body of rod (4) and the wide body of rod (5) of wing connection to wing It is integrally formed setting, and the longitudinal narrow body of rod (1), the wing longitudinally wide body of rod (2), the wing transverse direction body of rod (3), the wing of described wing Connect the narrow body of rod (4), wing connects the wide body of rod (5), three hollow out connecting rod A (8) and two hollow out connecting rod B (9) and adopted It is made of same material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720351774.8U CN206700758U (en) | 2017-04-05 | 2017-04-05 | A kind of wing of model aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720351774.8U CN206700758U (en) | 2017-04-05 | 2017-04-05 | A kind of wing of model aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206700758U true CN206700758U (en) | 2017-12-05 |
Family
ID=60467574
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720351774.8U Expired - Fee Related CN206700758U (en) | 2017-04-05 | 2017-04-05 | A kind of wing of model aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206700758U (en) |
-
2017
- 2017-04-05 CN CN201720351774.8U patent/CN206700758U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171205 Termination date: 20190405 |